CN210882654U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN210882654U CN210882654U CN201921942639.6U CN201921942639U CN210882654U CN 210882654 U CN210882654 U CN 210882654U CN 201921942639 U CN201921942639 U CN 201921942639U CN 210882654 U CN210882654 U CN 210882654U
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- battery
- groove
- connecting terminal
- unmanned aerial
- aerial vehicle
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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Abstract
The utility model discloses an unmanned aerial vehicle, which comprises a vehicle body and a battery, wherein a groove for accommodating the battery is arranged at the top of the vehicle body, a first connecting terminal is arranged in the groove, and a second connecting terminal matched with the first connecting terminal is arranged on the battery; the battery is characterized in that at least two convex strips are arranged on the inner side wall of the groove, a sliding groove matched with the convex strips is formed in the battery, and one elastic deformation layer is arranged on the surface of the sliding groove. The top of the machine body is provided with a groove for accommodating the battery, so that the battery cannot fall off from the machine body; the battery can be rapidly mounted and dismounted through the mutual matching of the convex strips and the sliding grooves; set up the elastic deformation layer on the surface of spout and can improve the connection stability between battery and the fuselage, the battery can stabilize the power supply, prevents the circumstances of outage from appearing in the flight process.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a stable unmanned vehicles of power supply.
Background
The battery of current unmanned vehicles sets up in the bottom of fuselage mostly, and it is troublesome either to install and dismantle, changes inconveniently, or is not good with mainboard connection stability, can lead to the outage at the flight in-process, takes place bad consequences such as crash.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the technical problem that will solve is: the unmanned aerial vehicle is stable in power supply and convenient to install and detach.
In order to solve the technical problem, the utility model discloses a technical scheme be:
an unmanned aerial vehicle comprises a vehicle body and a battery, wherein a groove for accommodating the battery is formed in the top of the vehicle body, a first connecting terminal is arranged in the groove, and a second connecting terminal matched with the first connecting terminal is arranged on the battery; the battery is characterized in that at least two convex strips are arranged on the inner side wall of the groove, a sliding groove matched with the convex strips is formed in the battery, and one elastic deformation layer is arranged on the surface of the sliding groove.
Furthermore, the elastic deformation layer is made of silicon rubber.
Further, still include the lamp body, the lamp body set up in the bottom of fuselage.
Furthermore, a heat dissipation structure is arranged at the top of the battery.
Further, the raised strips are in interference fit with the sliding grooves.
Furthermore, a concave position is arranged on the outer side wall of the battery.
The beneficial effects of the utility model reside in that: the top of the machine body is provided with a groove for accommodating the battery, so that the battery cannot fall off from the machine body; the battery can be rapidly mounted and dismounted through the mutual matching of the convex strips and the sliding grooves; set up the elastic deformation layer on the surface of spout and can improve the connection stability between battery and the fuselage, the battery can stabilize the power supply, prevents the circumstances of outage from appearing in the flight process.
Drawings
Fig. 1 is a schematic overall structure diagram of an unmanned aerial vehicle according to a first embodiment of the present invention;
fig. 2 is a schematic partial structural view of an unmanned aerial vehicle according to a first embodiment of the present invention;
fig. 3 is another schematic structural diagram of a portion of the unmanned aerial vehicle according to the first embodiment of the present invention.
Description of reference numerals:
1. a body; 11. a groove; 111. a convex strip; 12. a first connection terminal; 2. a battery; 21. a second connection terminal; 22. a chute; 3. and a lamp body.
Detailed Description
In order to explain the technical content, the objects and the effects of the present invention in detail, the following description is made with reference to the accompanying drawings in combination with the embodiments.
The utility model discloses the most crucial design lies in: the top of the machine body is provided with a groove for accommodating the battery, so that the battery cannot fall off from the machine body; through mutually supporting of sand grip and spout, can carry out the installation and the dismantlement of battery fast.
Referring to fig. 1 to 3, an unmanned aerial vehicle includes a body 1 and a battery 2, a groove 11 for accommodating the battery 2 is formed in the top of the body 1, a first connection terminal 12 is disposed in the groove 11, and a second connection terminal 21 matched with the first connection terminal 12 is disposed on the battery 2; be equipped with two at least sand grips 111 on the inside wall of recess 11, be equipped with on battery 2 with sand grip 111 matched with spout 22, the surface of spout 22 is equipped with one deck elastic deformation layer.
From the above description, the beneficial effects of the present invention are: the top of the machine body is provided with a groove for accommodating the battery, so that the battery cannot fall off from the machine body; the battery can be rapidly mounted and dismounted through the mutual matching of the convex strips and the sliding grooves; set up the elastic deformation layer on the surface of spout and can improve the connection stability between battery and the fuselage, the battery can stabilize the power supply, prevents the circumstances of outage from appearing in the flight process.
Furthermore, the elastic deformation layer is made of silicon rubber.
As can be seen from the above description, the silicone rubber has good deformability and is durable.
Further, still include lamp body 3, lamp body 3 set up in the bottom of fuselage 1.
As can be seen from the above description, the lamp body is arranged at the bottom of the unmanned aerial vehicle body, so that the unmanned aerial vehicle can be used for performing.
Further, a heat dissipation structure is arranged at the top of the battery 2.
Further, the protruding strip 111 is in interference fit with the sliding groove 22.
As can be seen from the above description, the interference fit may increase the connection stability.
Furthermore, a concave position is arranged on the outer side wall of the battery 2.
As can be seen from the above description, the provision of the recessed portion facilitates the handling during the removal of the battery.
Referring to fig. 1 to fig. 3, a first embodiment of the present invention is:
the utility model provides an unmanned vehicles, as shown in fig. 1 and 2, includes fuselage 1 and battery 2, the top of fuselage 1 is equipped with holds battery 2's recess 11, be equipped with first connecting terminal 12 in the recess 11, be equipped with two at least sand grip 111 on the inside wall of recess 11. As shown in fig. 3, be equipped with on battery 2 with first connecting terminal 12 matched with second connecting terminal 21, still be equipped with on battery 2 with sand grip 111 matched with spout 22, the surface of spout 22 is equipped with one deck elastic deformation layer, and is preferred, the material on elastic deformation layer is silicon rubber, sand grip 111 with spout 22 interference fit. In this embodiment, still be equipped with sunken position on the lateral wall of battery 2, the shape of sunken position can be designed into the shape that is close people's finger, is convenient for take off battery 2. The top of the battery 2 is provided with a heat dissipation structure which can be a heat dissipation strip or the like. The unmanned aerial vehicle further comprises a lamp body 3, and the lamp body 3 is arranged at the bottom of the vehicle body 1.
To sum up, the utility model provides a pair of unmanned vehicles, the installation of battery is dismantled conveniently, and the battery can stabilize the power supply, prevents the condition that the outage appears in the flight in-process.
The above mentioned is only the embodiment of the present invention, and not the limitation of the patent scope of the present invention, all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.
Claims (6)
1. An unmanned aerial vehicle comprises a vehicle body and a battery, and is characterized in that a groove for accommodating the battery is formed in the top of the vehicle body, a first connecting terminal is arranged in the groove, and a second connecting terminal matched with the first connecting terminal is arranged on the battery; the battery is characterized in that at least two convex strips are arranged on the inner side wall of the groove, a sliding groove matched with the convex strips is formed in the battery, and one elastic deformation layer is arranged on the surface of the sliding groove.
2. The UAV of claim 1 wherein the elastically deformable layer is made of silicone rubber.
3. The UAV of claim 1 further comprising a lamp body disposed at a bottom of the fuselage.
4. The UAV according to claim 1 wherein the battery is provided with a heat sink on top.
5. The UAV of claim 1 wherein the rib is an interference fit with the slot.
6. The UAV of claim 1 wherein the battery is recessed on an exterior sidewall of the battery.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921942639.6U CN210882654U (en) | 2019-11-11 | 2019-11-11 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921942639.6U CN210882654U (en) | 2019-11-11 | 2019-11-11 | Unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
CN210882654U true CN210882654U (en) | 2020-06-30 |
Family
ID=71340671
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201921942639.6U Active CN210882654U (en) | 2019-11-11 | 2019-11-11 | Unmanned aerial vehicle |
Country Status (1)
Country | Link |
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CN (1) | CN210882654U (en) |
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2019
- 2019-11-11 CN CN201921942639.6U patent/CN210882654U/en active Active
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